Vibration of thermally stressed composite cylinders

被引：2
|
作者：
Tenek, L [1 ]
机构：
[1] Univ Stuttgart, Inst Comp Applicat, D-70569 Stuttgart, Germany
来源：
AIAA JOURNAL | 1999年 / 37卷 / 11期
关键词：
D O I：
10.2514/2.632
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The effect of temperature in the fundamental natural frequency of laminated composite shells are investigated. The composite cylinder displays different fundamental frequencies for different laminations when thermally stressed. The quasi-isotropic composite cylindrical shell stiffens the most as a result of thermal stressing and represents an excellent design option at elevated environments.
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页码：1520 / 1521
页数：2
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